CN208149852U - A kind of aircraft box for exempting from bottom tongue - Google Patents
A kind of aircraft box for exempting from bottom tongue Download PDFInfo
- Publication number
- CN208149852U CN208149852U CN201820580589.0U CN201820580589U CN208149852U CN 208149852 U CN208149852 U CN 208149852U CN 201820580589 U CN201820580589 U CN 201820580589U CN 208149852 U CN208149852 U CN 208149852U
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- Prior art keywords
- plate
- tongue
- bottom plate
- aircraft box
- extension
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- 210000002105 tongue Anatomy 0.000 claims description 62
- 230000015572 biosynthetic process Effects 0.000 abstract description 6
- 238000004806 packaging method and process Methods 0.000 description 3
- 238000012856 packing Methods 0.000 description 3
- 238000000465 moulding Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 239000002390 adhesive tape Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
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- Packaging Of Machine Parts And Wound Products (AREA)
Abstract
The utility model belongs to the technical field of aircraft box, discloses a kind of aircraft box for exempting from bottom tongue.The aircraft box for exempting from bottom tongue includes top plate and the first bottom plate, the first tongue that top plate is outward extended with the first extension and connect with first extension；First bottom plate is oppositely arranged with the top plate, and first bottom plate is equipped with the first jack；First extension is bonded with the lower surface of first bottom plate, first tongue and the first jack grafting, and is located at first base plate interior.The first tongue connecting with top plate is plugged on the first jack on the first bottom plate by the utility model from outside to inside, so that the first tongue can be inserted the first jack and be located at the first base plate interior, so as to avoid the problem of after aircraft box assembled formation, the bottom of aircraft box can expose tongue and influence appearance.
Description
Technical field
The utility model relates to the technical field of aircraft box more particularly to a kind of aircraft boxes for exempting from bottom tongue.
Background technique
The corrugated case made of corrugated board, with its exclusive performance and advantage, in the competition with various packaging materials
In obtain great success, and be widely used in the packaging of various product.Aircraft box is a kind of typical corrugation packaging, because of it
Expansion exactly likes aircraft and gains the name, and is small courier packing, delivery first choice.
Increasingly attention with people to environmental protection, many brands pursue brief packaging, and the hand of retail is replaced with aircraft box
Work box is packed to reduce cost and unnecessary material consumption.Traditional aircraft box is defined as transportation and packing, because being assembled into
Need to improve the tongue insertion jack of left and right the stability of aircraft box when type.Publication No. CN203638270U's is practical new
Type patent discloses a kind of box-packaged case of aircraft, including：Bottom plate, front side board, back side panel, left plate, right side plate, top cover and envelope
Plate, the front side board, back side panel, left plate and right side plate are respectively arranged at the surrounding of bottom plate, and the side of the top cover is connected to
Back side panel, the other side are connected to sealing plate, are provided with adhesive tape and tear strip on the sealing plate.The packing box is needed in assembled formation
The tongue of left and right is inserted into jack, to improve the stability of aircraft box.But the shortcomings that technical solution is assembled formation
Aircraft cassette bottom portion afterwards can expose tongue, influence appearance.
It would therefore be highly desirable to need a kind of aircraft box of Novel free bottom tongue to solve the above problems.
Utility model content
The purpose of this utility model is to provide a kind of aircraft boxes for exempting from bottom tongue, to avoid in aircraft box assembled formation
Afterwards, the problem of bottom of aircraft box can expose tongue and influence appearance.
For this purpose, the utility model uses following technical scheme：
A kind of aircraft box for exempting from bottom tongue, including：
Top plate, the first tongue for being outward extended with the first extension and being connect with first extension；
First bottom plate is oppositely arranged with the top plate, and first bottom plate is equipped with the first jack；
First extension is bonded with the lower surface of first bottom plate, and first tongue and first jack are inserted
It connects, and is located at first base plate interior.
Preferably, further include the side plate positioned at first bottom plate two sides, each side plate includes and described the
Sequentially connected first side plate of one bottom plate and the second side plate, each second side plate are outward extended with the second extension, and two
A second extension mutually abuts, and is bonded with the upper surface of first bottom plate.
Preferably, each second extension is all provided with jagged, two notches are mutually abutted, and are set to described
The top of first jack.
Preferably, first bottom plate is outward extended with the second bottom plate, second bottom plate prolongs with two described second
The upper surface of extending portion is bonded.
Preferably, the two sides of second bottom plate are equipped with third side plate, the third side plate and second side plate are pasted
It closes.
Preferably, being equipped with back side panel between the top plate and first bottom plate, the both ends of the back side panel are set respectively
There is back side panel tongue, two back side panel tongues are plugged in respectively between first side plate and second side plate.
Preferably, second bottom plate is outward extended with third extension, the third extension and the back side panel
Fitting.
Preferably, front side board is connected between the top plate and first extension, the both ends point of the front side board
Not She You front side board tongue, two front side board tongues are plugged in respectively between first side plate and second side plate.
Preferably, second side plate is equipped with the second side plate tongue, the second side plate tongue and the front side board
Inner surface fitting.
Preferably, first tongue is equipped with the second jack, first jack is equipped with and the first bottom plate one
Molding second tongue, second jack and the second tongue grafting.
The beneficial effects of the utility model：
The first tongue connecting with top plate is plugged on first on the first bottom plate from outside to inside and inserted by the utility model
Hole, so that the first tongue can be inserted the first jack and be located at the first base plate interior, so as to avoid in aircraft box assembled formation
Afterwards, the problem of bottom of aircraft box can expose tongue and influence appearance.
Detailed description of the invention
Fig. 1 is the expanded view of the aircraft box provided by the utility model for exempting from bottom tongue；
Fig. 2 is one and half expanded views of the aircraft box provided by the utility model for exempting from bottom tongue；
Fig. 3 is another half expanded view of the aircraft box provided by the utility model for exempting from bottom tongue；
Fig. 4 is the bottom view after the aircraft box folding forming provided by the utility model for exempting from bottom tongue.
In figure：
1, top plate；11, the first extension；12, the first tongue；13, the second jack；14, front side board；15, front side board tongue；
2, the first bottom plate；21, the first jack；22, the second tongue；23, back side panel；24, back side panel tongue；
31, the first side plate；32, the second side plate；33, the second side plate tongue；34, the second extension；35, notch；
4, the second bottom plate；41, third side plate；42, third extension.
Specific embodiment
Further illustrate the technical solution of the utility model below with reference to the accompanying drawings and specific embodiments.
As shown in Figure 1, a kind of expanded view of aircraft box for exempting from bottom tongue provided by the utility model, the aircraft box include
Top plate 1, the first bottom plate 2, side plate and the second bottom plate 4, top plate 1, side plate and the second bottom plate 4 are connect with the first bottom plate 2, wherein：
Top plate 1 is connect by back side panel 23 with the first bottom plate 2, and the both ends of back side panel 23 are respectively equipped with back side panel tongue 24；
Side plate is located at the two sides of the first bottom plate 2, and each side plate includes sequentially connected first side plate 31 of the first bottom plate 2 and second side
Plate 32；When folding, the first side plate 31 and the second side plate 32 are folded and form side plate, back side panel tongue 24 is plugged on the first side plate
31 and second between side plate 32, so that the intensity of side plate further enhances.
Each second side plate 32 is outward extended with the second extension 34, and two the second extensions 34 mutually abut, specifically
Ground is that the side of two the second extensions 34 mutually abuts, and is bonded with the upper surface of the first bottom plate 2, is further increased in this way
The structural strength of strong first bottom plate 2, while two the second extensions 34 form mutual support structure, can further ensure aircraft
The stability of box.
Each second extension 34 is all provided with jagged 35, and two notches 35 mutually abut, and are set to the upper of the first jack 21
Side, the space that two notches 35 are formed, which is formed, allows bit space, and one and half expanded views of aircraft box refer to Fig. 2 at this time.
First bottom plate 2 is outward extended with the second bottom plate 4, and the second bottom plate 4 is bonded with the upper surface of two the second extensions 34,
Second bottom plate 4 is further fitted in two the second extensions 34 after two the second extensions 34 are fitted on the first bottom plate 2
On, the structural strength of the first bottom plate 2 can be further enhanced.The two sides of the second bottom plate 4 are equipped with third side plate 41, third side simultaneously
Plate 41 is bonded with the second side plate 32, can further enhance the structural strength of side plate.The second bottom plate 4 is outward extended with third simultaneously
Extension 42, third extension 42 are bonded with back side panel 23, can further enhance the structural strength of back side panel 23, at this time aircraft
Another half expanded view of box refers to Fig. 3.
Specifically, the first tongue 12 that top plate 1 is outward extended with the first extension 11 and connect with the first extension 11, top
Front side board 14 is connected between plate 1 and the first extension 11, the both ends of front side board 14 are respectively equipped with front side board tongue 15, by top plate
1 is turned over downwards, and the first extension 11 is bonded with the lower surface of the first bottom plate 2, and makes 21 grafting of the first tongue 12 and the first jack,
Two front side board tongues 15 are plugged in respectively between the first side plate 31 and the second side plate 32, so as to further enhance side plate
Structural strength, entire aircraft box is fully folded as type at this time, the bottom view of aircraft box after molding as shown in Figure 4.And front side
For plate 14 after fold, cooperation and the second side plate tongue 33 on the second side plate 32 make the second side plate tongue 33 and front side board 14
Inner surface fitting, it follows that the second side plate tongue 33 can not only block the article being placed in the second bottom plate 4, while can
To further enhance the structural strength of front side board 14.
Referring to Fig. 4, the first tongue 12 is equipped with the second jack 13, the first jack 21 is equipped with to be integrally formed with the first bottom plate 2
The second tongue 22, pass through utilize the first tongue 12 and 21 grafting of the first jack, and utilization the second jack 13 and the second tongue
Double inserting modes of 22 grafting, it is ensured that the stability and protectiveness of aircraft box grafting.
To sum up, the first tongue 12 connecting with top plate 1 is plugged on the first bottom plate 2 by the utility model from outside to inside
The first jack 21 so that the first tongue 12 can be inserted the first jack 21 and be located at the first bottom plate 2 inside, so as to avoid
After aircraft box assembled formation, the problem of bottom of aircraft box can expose tongue and influence appearance.It is simultaneously the secured of guarantee grafting
Degree, aircraft box design double inserting modes of the second jack 13 and 22 grafting of the second tongue, so that structure is more compact and stablizes.
Obviously, the above embodiments of the present invention is used for the purpose of clearly illustrating examples for clearly illustrating the present invention, and
It is not limitations of the embodiments of the present invention.For the ordinary skill user of fields, in above description
On the basis of can also make other variations or changes in different ways.There is no need and unable to give all embodiments
Exhaustion.Any modifications, equivalent replacements, and improvements made within the spirit and principle of the present invention etc., should be included in
Within the protection scope of the utility model claims.
Claims (10)
1. a kind of aircraft box for exempting from bottom tongue, which is characterized in that including：
Top plate (1), the first tongue for being outward extended with the first extension (11) and being connect with first extension (11)
(12)；
First bottom plate (2) is oppositely arranged with the top plate (1), and first bottom plate (2) is equipped with the first jack (21)；
First extension (11) is bonded with the lower surface of first bottom plate (2), first tongue (12) and described the
One jack (21) grafting, and it is internal to be located at first bottom plate (2).
2. aircraft box according to claim 1, which is characterized in that further include positioned at the side of the first bottom plate (2) two sides
Plate, each side plate include with sequentially connected first side plate (31) of first bottom plate (2) and the second side plate (32), often
A second side plate (32) is outward extended with the second extension (34), and two second extensions (34) mutually abut,
And it is bonded with the upper surface of first bottom plate (2).
3. aircraft box according to claim 2, which is characterized in that each second extension (34) is all provided with jagged
(35), two notches (35) mutually abut, and are set to the top of first jack (21).
4. aircraft box according to claim 2, which is characterized in that first bottom plate (2) is outward extended with the second bottom plate
(4), second bottom plate (4) is bonded with the upper surface of two second extensions (34).
5. aircraft box according to claim 4, which is characterized in that the two sides of second bottom plate (4) are equipped with third side plate
(41), the third side plate (41) is bonded with second side plate (32).
6. aircraft box according to claim 4, which is characterized in that set between the top plate (1) and first bottom plate (2)
Have back side panel (23), the both ends of the back side panel (23) are respectively equipped with back side panel tongue (24), two back side panel tongues
(24) it is plugged in respectively between first side plate (31) and second side plate (32).
7. aircraft box according to claim 6, which is characterized in that second bottom plate (4) is outward extended with third extension
Portion (42), the third extension (42) are bonded with the back side panel (23).
8. aircraft box according to claim 2, which is characterized in that the top plate (1) and first extension (11) it
Between be connected with front side board (14), the both ends of the front side board (14) are respectively equipped with front side board tongue (15), two front side boards
Tongue (15) is plugged in respectively between first side plate (31) and second side plate (32).
9. aircraft box according to claim 8, which is characterized in that second side plate (32) is equipped with the second side plate tongue
(33), the second side plate tongue (33) is bonded with the inner surface of the front side board (14).
10. aircraft box described according to claim 1~any one of 9, which is characterized in that first tongue (12) is equipped with the
Two jacks (13), first jack (21) be connected with integrally formed second tongue (22) of first bottom plate (2), it is described
Second jack (13) and second tongue (22) grafting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820580589.0U CN208149852U (en) | 2018-04-23 | 2018-04-23 | A kind of aircraft box for exempting from bottom tongue |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820580589.0U CN208149852U (en) | 2018-04-23 | 2018-04-23 | A kind of aircraft box for exempting from bottom tongue |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208149852U true CN208149852U (en) | 2018-11-27 |
Family
ID=64378841
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820580589.0U Active CN208149852U (en) | 2018-04-23 | 2018-04-23 | A kind of aircraft box for exempting from bottom tongue |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208149852U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108438419A (en) * | 2018-04-23 | 2018-08-24 | 恒铭达包装材料（惠州）有限公司 | A kind of aircraft box for exempting from bottom tongue |
-
2018
- 2018-04-23 CN CN201820580589.0U patent/CN208149852U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108438419A (en) * | 2018-04-23 | 2018-08-24 | 恒铭达包装材料（惠州）有限公司 | A kind of aircraft box for exempting from bottom tongue |
| CN108438419B (en) * | 2018-04-23 | 2024-10-22 | 恒铭达包装材料（惠州）有限公司 | Bottom-insertion-free aircraft box |
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